Orbit space transportation & recovery system

a technology for orbital positioning and recovery, applied in the field of spacecraft and satellites, can solve the problems of many millions of dollars in the space of satellite placement, and achieve the effects of reducing the cost of changing the orbital position of a satellite, reducing the cost of space exploration, and revolutionizing the commercial space industry

Inactive Publication Date: 2007-02-22
IOSTAR CORP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

[0030] The development of an in-orbit space transportation and rescue vehicle would dramatically reduce the cost of changing the orbital position of a satellite. Such a system would revolutionize the military and commercial space industries, and fill a long-felt need in the telecommunications, direct-broadcast and remote-sensing industries.
[0031] The In Orbit Space Transportation & Recovery System (IOSTAR™) will revolutionize the commercial space industry by providing a lower cost alternative to conventional methods of moving spacecraft in orbit. Instead of usi

Problems solved by technology

The placement of satellites into Earth

Method used

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  • Orbit space transportation & recovery system
  • Orbit space transportation & recovery system
  • Orbit space transportation & recovery system

Examples

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Embodiment Construction

I. Overview of Embodiments of IOSTAR™

[0051]FIGS. 1A and 1B reveal side and end views of one of the preferred embodiments of the In Orbit Transportation & Recovery System, or IOSTAR™10. IOSTAR™ is a Trade and Service Mark owned by the Assignee. IOSTAR™ is a reusable spacecraft 10 which is designed primarily for orbital transportation and rescue services.

[0052] In this Specification and in the Claims that follow, the term “satellite” refers to any object in any orbit around anybody, whether natural or man-made. Any object which remains above the Earth's atmosphere for an extended time is a satellite, since it must be within the gravitational influence of the Earth or some other celestial body. A “celestial body” is any planet, moon, asteroid, comet, star, galaxy, or any other aggregation of matter. The terms “vehicle” and “spacecraft” concerns any man-made device or means used temporarily below orbital altitude, in orbit, or beyond the Earth's atmosphere, or for travel in space; incl...

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PUM

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Abstract

An In Orbit Transportation & Recovery System (IOSTAR™) (10). One preferred embodiment of the present invention comprises a space tug powered by a nuclear reactor (19). The IOSTAR™ includes a collapsible boom (11) connected at one end to a propellant tank (13) which stores fuel for an electric propulsion system (12). This end of the boom (11) is equipped with docking hardware (14) that is able to grasp and hold a satellite (15) and as a means to refill the tank (13). Radiator panels (16) mounted on the boom (11) dissipate heat from the reactor (19). A radiation shield (20) is situated next to the reactor (19) to protect the satellite payload (15) at the far end of the boom (11). The IOSTAR™ (10) will be capable of accomplishing rendezvous and docking maneuvers which will enable it to move spacecraft between a low Earth parking orbit and positions in higher orbits or to other locations in our Solar System.

Description

CROSS-REFERENCE TO RELATED PENDING PATENT APPLICATIONS & CLAIMS FOR PRIORITY [0001] The Present patent application is a Non-Provisional, Continuation-in-Part patent application. The Applicants claim the benefit of priority under Sections 119 & 120 for any subject matter which is commonly disclosed in the Present application and in: [0002] Pending U.S. patent application IOS9601CIPC, Ser. No. 10 / 755,200, filed on 9 Jan. 2004; [0003] Pending U.S. patent application IOS9601CIPB, Ser. No. 10 / 736,887, filed on 15 Dec. 2003; [0004] Pending PCT International Patent Application IOS9601-B&C-PCT, PCT / GB04 / ______, filed on 29 Jan. 2004; [0005] Pending PCT International Patent Application ITS9601-CIPB-PCT, PCT / US03 / 32748, filed on 10 Nov. 2003; [0006] Abandoned U.S. patent application ITS9601 CIPA, U.S. Ser. No. 10 / 298,138, filed on 15 Nov. 2002; and [0007] Abandoned U.S. patent application ITS9601, U.S. Ser. No. 09 / 918,705, filed on 30 Jul. 2001.FIELD OF THE INVENTION [0008] The present invent...

Claims

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Application Information

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IPC IPC(8): B64G1/64
CPCB64G1/007B64G1/1078B64G1/405B64G1/408B64G1/422B64G1/503G21Y2004/30B64G1/54B64G1/646G21D5/02G21Y2002/203G21Y2002/304B64G1/506Y02E30/00B64G1/2427
Inventor D'AUSILIO, ROBERT F.STUART, JAMES R.WILLIAMS, FRANKLIN H. JR.GIACCHERINI, THOMAS N.
Owner IOSTAR CORP
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